GB1347078A - Transponder beacons - Google Patents
Transponder beaconsInfo
- Publication number
- GB1347078A GB1347078A GB4553871A GB4553871A GB1347078A GB 1347078 A GB1347078 A GB 1347078A GB 4553871 A GB4553871 A GB 4553871A GB 4553871 A GB4553871 A GB 4553871A GB 1347078 A GB1347078 A GB 1347078A
- Authority
- GB
- United Kingdom
- Prior art keywords
- phase
- inputs
- signals
- received
- outputs
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 230000010287 polarization Effects 0.000 abstract 7
- 230000001427 coherent effect Effects 0.000 abstract 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q15/00—Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
- H01Q15/14—Reflecting surfaces; Equivalent structures
- H01Q15/22—Reflecting surfaces; Equivalent structures functioning also as polarisation filter
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/74—Systems using reradiation of radio waves, e.g. secondary radar systems; Analogous systems
- G01S13/76—Systems using reradiation of radio waves, e.g. secondary radar systems; Analogous systems wherein pulse-type signals are transmitted
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
- G01S7/02—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
- G01S7/024—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00 using polarisation effects
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q21/00—Antenna arrays or systems
- H01Q21/24—Combinations of antenna units polarised in different directions for transmitting or receiving circularly and elliptically polarised waves or waves linearly polarised in any direction
- H01Q21/245—Combinations of antenna units polarised in different directions for transmitting or receiving circularly and elliptically polarised waves or waves linearly polarised in any direction provided with means for varying the polarisation
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- Computer Networks & Wireless Communication (AREA)
- General Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
1347078 Aerials; radar; transponder apparatus INTERNATIONAL STANDARD ELECTRIC CORP 30 Sept 1971 [8 Oct 1970] 45538/71 Headings H4A H4D and H4L A beacon for use in conjunction with coherent pulse Doppler radars is arranged to retransmit signals which have polarizations corresponding to those of received signals. An aerial system is provided which has two orthogonally polarized components. As described (Fig. 3, not shown) twelve lengths of waveguide are placed side-byside with their upper faces lying in a common plane. Said upper faces each carry an array of parallel dipoles or of slots which are disposed at - 45 degrees to the waveguide axis in odd-numbered waveguides, and at +45 degrees to the waveguide axis in even-numbered waveguides. A series of couplers connects the odd-numbered waveguides to a terminal G, and another series of couplers connects the even numbered waveguides to a terminal D. The said terminals are connected through respective pairs of directional couplers 8, 10 and 9, 11, Fig. 2, and respective electronically controlled phase shifters 16, 17 to respective short circuits 18, 19. The directional couplers 8, 9 apply small portions of the received energies through respective amplifier/ detectors 12, 13 to first and second inputs H1, H2 of a logic circuit 21. The directional couplers 10, 11 are connected to the inputs of a hybrid junction 20, the outputs B, A of which are connected through respective amplifier/detectors 14, 15 to third and fourth inputs H3, H4 of the logic circuit 21. A circuit 25 is connected to the outputs (five) of the logic circuit 21 and controls the operations of two sawtooth generators 22, 23 associated with respective phase shifters 16, 17. The relative phases of the received energies at the array terminals D, G depend upon the kind of polarization of the impinging waves, being in phase for vertical polarization, in anti-phase for horizontal polarization, and in quadrature for circular polarization. The hybrid junction 20 provides respectively to its outputs A, B signals in phase and in anti-phase with respect to the input signals. With equal in phase inputs, there is output only at A. If the inputs are in anti-phase, there is output only at B. If the inputs are in quadrature, there are outputs both at A and B. The phase shifters 16, 17 have ranges of 0 to # and, since they are traversed twice by the signals provide a maximum phase change of 2#. They are not operated unless the received signals exceed a predetermined threshold value. The sawtooth repetition frequency represents a Doppler frequency which is assigned to the particular beacon. The following table shows whether there are (1), or are not (0), signals to the inputs of the logic circuit 21 for the various received polarizations, and which of the sawtooth generators 22, 23 are operated With circular polarization it is arranged that the re-transmitted waves are of opposite hand from that of the received waves.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7036372A FR2108814B1 (en) | 1970-10-08 | 1970-10-08 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1347078A true GB1347078A (en) | 1974-02-13 |
Family
ID=9062466
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4553871A Expired GB1347078A (en) | 1970-10-08 | 1971-09-30 | Transponder beacons |
Country Status (3)
Country | Link |
---|---|
US (1) | US3716856A (en) |
FR (1) | FR2108814B1 (en) |
GB (1) | GB1347078A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2165413A (en) * | 1982-06-18 | 1986-04-09 | Dornier System Gmbh | Generating artificial target marks in an SAR display |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3883872A (en) * | 1973-06-28 | 1975-05-13 | Nasa | System for interference signal nulling by polarization adjustment |
US4035797A (en) * | 1975-11-14 | 1977-07-12 | General Motors Corporation | Polarized radar system for providing target identification and discrimination |
US4197541A (en) * | 1977-12-19 | 1980-04-08 | International Telephone And Telegraph Corporation | Polarization agile planar array |
US4159475A (en) * | 1978-06-05 | 1979-06-26 | Calspan Corporation | VCO-Controlled phase lock system |
US4218680A (en) * | 1979-01-12 | 1980-08-19 | Motorola, Inc. | Coded coherent transponder |
US4293858A (en) * | 1979-11-23 | 1981-10-06 | International Telephone And Telegraph Corporation | Polarization agile meander line array |
US4670753A (en) * | 1984-10-01 | 1987-06-02 | The Boeing Company | Method and apparatus for minimum amplitude time history analysis |
FR2643726B1 (en) * | 1989-02-27 | 1992-01-31 | Caro Line Habigand | CONTACTLESS IDENTIFICATION SYSTEM OF A MOBILE MOVING NEAR A FIXED STATION |
JP2735758B2 (en) * | 1992-11-25 | 1998-04-02 | 防衛庁技術研究本部長 | Method for compensating fluctuation of synthetic aperture radar and position measurement method using radar |
US10852390B2 (en) * | 2017-12-20 | 2020-12-01 | Waymo Llc | Multiple polarization radar unit |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2683855A (en) * | 1949-11-30 | 1954-07-13 | Raytheon Mfg Co | Frequency converter |
US3146447A (en) * | 1962-07-17 | 1964-08-25 | Harold L Newman | Communication system |
US3331070A (en) * | 1966-01-12 | 1967-07-11 | Donald J Sommers | Radar moving target simulator |
-
1970
- 1970-10-08 FR FR7036372A patent/FR2108814B1/fr not_active Expired
-
1971
- 1971-09-30 GB GB4553871A patent/GB1347078A/en not_active Expired
- 1971-10-06 US US00186899A patent/US3716856A/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2165413A (en) * | 1982-06-18 | 1986-04-09 | Dornier System Gmbh | Generating artificial target marks in an SAR display |
Also Published As
Publication number | Publication date |
---|---|
FR2108814A1 (en) | 1972-05-26 |
US3716856A (en) | 1973-02-13 |
FR2108814B1 (en) | 1976-09-03 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
435 | Patent endorsed 'licences of right' on the date specified (sect. 35/1949) | ||
PCNP | Patent ceased through non-payment of renewal fee |